RU2196703C2 - Летательный аппарат с фюзеляжем, выполненным по существу в виде аэростатического подъемного тела, двигательная установка и способ управления летательным аппаратом - Google Patents

Летательный аппарат с фюзеляжем, выполненным по существу в виде аэростатического подъемного тела, двигательная установка и способ управления летательным аппаратом Download PDF

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Publication number
RU2196703C2
RU2196703C2 RU99114030/28A RU99114030A RU2196703C2 RU 2196703 C2 RU2196703 C2 RU 2196703C2 RU 99114030/28 A RU99114030/28 A RU 99114030/28A RU 99114030 A RU99114030 A RU 99114030A RU 2196703 C2 RU2196703 C2 RU 2196703C2
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Russia
Prior art keywords
propeller
shaft
rotation
aircraft according
aircraft
Prior art date
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RU99114030/28A
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English (en)
Russian (ru)
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RU99114030A (ru
Inventor
Херманн КЮНКЛЕР
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Херманн КЮНКЛЕР
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/125—Arrangements on vessels of propulsion elements directly acting on water of propellers movably mounted with respect to hull, e.g. adjustable in direction, e.g. podded azimuthing thrusters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/24—Arrangement of propulsion plant
    • B64B1/30—Arrangement of propellers
    • B64B1/32—Arrangement of propellers surrounding hull
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/52—Tilting of rotor bodily relative to fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B2201/00—Hybrid airships, i.e. airships where lift is generated aerodynamically and statically

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Ocean & Marine Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Elimination Of Static Electricity (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
  • Transmission Devices (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Fuses (AREA)
  • Handcart (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Motor Power Transmission Devices (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
RU99114030/28A 1997-01-04 1998-01-02 Летательный аппарат с фюзеляжем, выполненным по существу в виде аэростатического подъемного тела, двигательная установка и способ управления летательным аппаратом RU2196703C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19700182.3 1997-01-04
DE19700182A DE19700182A1 (de) 1997-01-04 1997-01-04 Luftfahrzeug mit einem im wesentlichen als aerostatischem Auftriebskörper ausgebildeten Rumpf

Publications (2)

Publication Number Publication Date
RU99114030A RU99114030A (ru) 2001-03-27
RU2196703C2 true RU2196703C2 (ru) 2003-01-20

Family

ID=7816849

Family Applications (1)

Application Number Title Priority Date Filing Date
RU99114030/28A RU2196703C2 (ru) 1997-01-04 1998-01-02 Летательный аппарат с фюзеляжем, выполненным по существу в виде аэростатического подъемного тела, двигательная установка и способ управления летательным аппаратом

Country Status (19)

Country Link
US (2) US6286783B1 (de)
EP (2) EP0948441B1 (de)
JP (1) JP2001507306A (de)
CN (2) CN1085973C (de)
AT (2) ATE328787T1 (de)
AU (1) AU717125B2 (de)
BR (1) BR9806838A (de)
CA (1) CA2276876A1 (de)
CZ (1) CZ233299A3 (de)
DE (3) DE19700182A1 (de)
DK (1) DK0948441T3 (de)
ES (1) ES2185145T3 (de)
ID (1) ID21900A (de)
IL (1) IL130655A (de)
PL (1) PL334353A1 (de)
PT (1) PT948441E (de)
RU (1) RU2196703C2 (de)
UA (1) UA49050C2 (de)
WO (1) WO1998029303A2 (de)

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US8297550B2 (en) 2007-08-09 2012-10-30 Lta Corporation Lenticular airship and associated controls
USD670638S1 (en) 2010-07-20 2012-11-13 Lta Corporation Airship
US8596571B2 (en) 2011-03-31 2013-12-03 Lta Corporation Airship including aerodynamic, floatation, and deployable structures
WO2014168511A1 (ru) * 2013-04-12 2014-10-16 Общество с ограниченной ответственностью ОКБ "АТЛАНТ" Силовая установка с изменяемым вектором тяги
US8894002B2 (en) 2010-07-20 2014-11-25 Lta Corporation System and method for solar-powered airship
RU2550797C1 (ru) * 2014-04-09 2015-05-10 Рудольф Львович Гроховский Дирижабль
WO2016022040A1 (ru) * 2014-08-05 2016-02-11 Ардн Технолоджи Лимитед Аэромобиль
US9802690B2 (en) 2013-11-04 2017-10-31 Lta Corporation Cargo airship
RU2642210C1 (ru) * 2016-12-22 2018-01-24 Александр Александрович Перфилов Воздухоплавательный аппарат
RU2652373C1 (ru) * 2017-05-31 2018-04-25 Александр Александрович Перфилов Воздухоплавательный аппарат
RU2684813C1 (ru) * 2018-02-19 2019-04-15 Дмитрий Атбашьян Узел подвешивания и регулирования угла вектора тяги двигателя

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CA2276876A1 (en) 1998-07-09
WO1998029303A8 (de) 1999-11-11
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PT948441E (pt) 2003-02-28
CN1123486C (zh) 2003-10-08
IL130655A0 (en) 2000-06-01
DE19700182A1 (de) 1998-07-09
JP2001507306A (ja) 2001-06-05
ES2185145T3 (es) 2003-04-16
ATE328787T1 (de) 2006-06-15
CN1249720A (zh) 2000-04-05
BR9806838A (pt) 2000-03-14
DK0948441T3 (da) 2003-02-03
IL130655A (en) 2003-04-10
AU6206998A (en) 1998-07-31
WO1998029303A2 (de) 1998-07-09
US6467724B2 (en) 2002-10-22
EP1160156A3 (de) 2003-05-21
WO1998029303A3 (de) 1998-11-05
EP0948441A2 (de) 1999-10-13
CN1085973C (zh) 2002-06-05
PL334353A1 (en) 2000-02-28
WO1998029303B1 (de) 1999-10-07
CZ233299A3 (cs) 1999-12-15
US6286783B1 (en) 2001-09-11
UA49050C2 (uk) 2002-09-16
EP0948441B1 (de) 2002-10-02
EP1160156B1 (de) 2006-06-07
DE59805790D1 (de) 2002-11-07
DE59813586D1 (de) 2006-07-20
ATE225279T1 (de) 2002-10-15
AU717125B2 (en) 2000-03-16
CN1392083A (zh) 2003-01-22
ID21900A (id) 1999-08-12

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